Padma, Madhuranath and Rekha, R and Srinathkumar, S (1991) Linear Models For The - LCA 645-33. Technical Report. NAL, Bangalore.
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Abstract
The Stability Analysis And Control Law Design Of The Contemplated Light Combat Aircraft Needs Derivation Of Linear Aircraft Models From Non-Linear Flight Simulation Models . This Document Presents The Linear Longitudinal And Lateral State And Observation Models-Of The LCA Version 645-33 Obtained From NAL Developed Software For A Dozen Representative Conditions In The Flight Envelope . Poles And Zeros Of The Corresponding - Transfer Functions Have Been Generated And Compared With Those. Obtained By The Aircraft Prime.The Comparisons Give Confidence In The Use Of The Models Obtained From The NAL . Software For Control Law Design.
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Linear Models; Combat Aircraft; -Flight Simulation; Control Law Design Aid |
| Subjects: | ASTRONAUTICS > Astronautics (General) |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 24 Aug 2012 04:35 |
| Last Modified: | 24 Aug 2015 09:50 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10777 |
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